US9297423B2ActiveUtilityA1

Stator coupling

Assignee: SICK STEGMANN GMBHPriority: Jul 31, 2012Filed: Jul 16, 2013Granted: Mar 29, 2016
Est. expiryJul 31, 2032(~6 yrs left)· nominal 20-yr term from priority
Y10T403/45G01D 5/24442F16D 1/12G01D 5/347Y10T403/64F16B 2200/50
52
PatentIndex Score
2
Cited by
12
References
14
Claims

Abstract

A stator coupling for the torsionally rigid connection of two components allows radial and axial relative movements within tolerance limits has a base surface ( 10 ) with first ( 18.1, 18.2 ) and second ( 28 ) lugs. The second lugs ( 28 ) are positioned at the straight-line edges between the assembly points ( 26, 42 ). Bent edges ( 30, 32 ) parallel to one respective edge are bent away at least twice, so that a flange ( 34.1, 34.2, 34.3, 34.4 ) surface-parallel to the base surface ( 10 ) is formed. Two second lugs, are positioned at edges following one another in the peripheral direction, and overlap with mutually facing ends of their flanges and these ends each together form one of a set of second assembly points ( 42.1, 42.2 ).

Claims

exact text as granted — not AI-modified
The invention claimed is: 
     
       1. A stator coupling for the torsionally rigid connection of two components which allows radial and axial relative movements within tolerance limits, the stator coupling comprising:
 a planar base surface ( 10 ); 
 first lugs ( 18 . 1 ,  18 . 2 ) which are positioned at the base surface ( 10 ) and which have a pair of first assembly points ( 26 . 1 ,  26 . 2 ) arranged diametrical with respect to one another in a first axis for fastening to the one component, the first axis is an X axis; 
 second lugs ( 28 ) which are positioned at the base surface ( 10 ) and are bent out of the plane of the base surface ( 10 ) and which have a pair of second assembly points ( 42 . 1 ,  42 . 2 ) arranged diametrical with respect to one another in a second axis for fastening to the other component, the second axis is a Y axis, 
 wherein the first axis and the second axis extend approximately perpendicular to one another in the plane of the base surface ( 10 ) and wherein the base surface ( 10 ) has a polygonal contour and has respective straight-line edges between the first assembly points and the second assembly points ( 26 ,  42 ), 
 the second lugs ( 28 . 1 ,  28 . 2 ,  28 . 3 ,  28 . 4 ) are positioned at the straight-line edges of the base surface ( 10 ) and bent edges ( 30 ,  32 ) parallel to the respective edge are bent away at least twice, whereby a flange ( 34 . 1 ,  34 . 2 ,  34 . 3 ,  34 . 4 ) surface-parallel to the base surface ( 10 ) is formed, 
 and two respective second lugs ( 28 . 1  and  28 . 2  or  28 . 3  and  28 . 4  respectively), which are positioned at edges following one another in the peripheral direction, overlap with the mutually facing ends of their flanges ( 34 . 1  and  34 . 2  or  34 . 3  and  34 . 4  respectively) and these ends each together have one of the second assembly points ( 42 . 1  and  42 . 2  respectively). 
 
     
     
       2. The stator coupling in accordance with  claim 1 , wherein the first lugs are bent away perpendicular out of the plane of the base surface. 
     
     
       3. The stator coupling in accordance with  claim 1 , wherein the first lugs are inwardly or outwardly angled so that they have a flange for the assembly points which is surface-parallel to the plane of the base surface. 
     
     
       4. The stator coupling in accordance with  claim 1 , wherein the first lugs ( 18 . 1 ,  18 . 2 ) start at two mutually oppositely disposed parallel sides of the base surface ( 10 ); and wherein the second lugs ( 28 . 1 ,  28 . 2  and  28 . 3 ,  28 . 4  respectively) are positioned at the sides of the base surface ( 10 ) contacting one another at two mutually opposite corners. 
     
     
       5. The stator coupling in accordance with  claim 1 , wherein the base surface ( 10 ) has a hexagonal contour. 
     
     
       6. The stator coupling in accordance with  claim 1 , wherein the base surface ( 10 ) has a respective material-reduced desired bending point between the first lugs ( 18 . 1  or  18 . 2  respectively) and the second lugs ( 28 . 1  and  28 . 3  or  28 . 2  and  28 . 4  respectively). 
     
     
       7. The stator coupling in accordance with  claim 6 , wherein the material-reduced desired bending point is respectively formed by indentations ( 44 ) arranged at both sides of the first lugs ( 18 . 1 ,  18 . 2 ) which indentations reduce the material width of the base surface ( 10 ). 
     
     
       8. The stator coupling in accordance with  claim 1 , wherein the base surface ( 10 ) is manufactured with the first lugs ( 18 ) and second lugs ( 28 ) positioned at it as a single-piece stamped bent part or as a single-piece laser welded part. 
     
     
       9. The stator coupling in accordance with  claim 1 , wherein the first lugs ( 18 ) and/or the second lugs ( 28 ) are manufactured separately and are fastened to the base surface ( 10 ). 
     
     
       10. The stator coupling in accordance with  claim 1 , wherein the first lugs ( 18 ) and/or the second lugs ( 28 ) are manufactured separately and are welded to the base surface ( 10 ). 
     
     
       11. The stator coupling in accordance with  claim 1 , wherein the flanges ( 34 ) of the second lugs ( 28 ) have surface openings ( 36 ) for a mass reduction. 
     
     
       12. The stator coupling in accordance with  claim 1 , wherein the second lugs ( 28 ) start at straight-line outer edges of the base surface ( 10 ). 
     
     
       13. The stator coupling in accordance with  claim 1 , wherein the second lugs ( 28 ) are bent to form a U-shaped or C-shaped section open toward the center of the stator coupling. 
     
     
       14. The stator coupling in accordance with  claim 1 , wherein the second lugs ( 28 ) extend from the respective second assembly point ( 42 ) as a planar surface up to the respective adjacent first lug ( 18 ).

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